THE matrix flexibility method for the prediction of the normal modes of vibration of a structure may be extended to the case of a structure which has no external supports. This is of particular relevance to problems of aircraft and missile vibration.
Natural Vibrations of a Free Structure
Application of the Matrix Flexibility Method to the Prediction of Normal Vibration Modes Using a Co-ordinate System Which Facilitates Programming on a Digital Computer
Aircraft Engineering and Aerospace Technology ; 34 , 3 ; 81-83
1962-03-01
3 pages
Article (Journal)
Electronic Resource
English
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